Apparatus and method of sampling semivolatile compounds

ABSTRACT

An apparatus and method for sampling semivolatile compounds is disclosed. A collection bag is placed around an air conditioning vent on an aircraft. An opening in the collection bag receives air from the air conditioning vent into the bag. An exit in the collection bag allows the air sample to escape from the collection bag. Vacuum applied by tubing at the exit pulls the air sample from the bag. Flow is adjusted so that the inflow into the collection bag exceeds the outtake, thereby inflating the bag. The inflation of the collection bag assures that the air being sampled is only air originating from the air conditioning vent.

This application is related to U.S. patent application No. entitled“High Volume Air Sampler and Pressure Reduction Apparatus And Method.”

FIELD OF THE INVENTION

The present invention relates to air sampling. More particularly theinvention relates to methods and equipment used for taking air samplesfrom an enclosed volume such as that encountered in an aircraft cabin.In particular the present invention also relates to an air samplingtrain, adapters, and associated ductwork for receiving an air samplefrom an aircraft air conditioning vent.

BACKGROUND OF THE INVENTION

Air samplers are finding increased application in a variety of uses. Onesuch application deals with the transportation industry. For example,passengers may be subject to noxious smells or gases or other airborneimpurities when traveling in enclosed vehicles such as trains, motorcoaches, or airplanes.

When an event occurs during which passengers are subject to odors,smoke, gases, or other undesirable airborne impurities, it is desirableto perform some kind of test or sampling. The testing or sampling of theair supply may be done for several reasons. It may be desired to repeatthe incident of impure air flow in order to sample the air and thustrace the source of impurity. Additionally, the testing or sampling maybe performed in part to certify that, once corrected, the vehicle inquestion is again supplying clean air to passengers.

In the example of a modern passenger jetliner, air supply to theinterior cabin often begins with the gas turbine engines. In the typicalstructure of a gas turbine engine, including those used in industrial,marine, vehicle, as well as aerojet applications, air enters the engineinlet and first passes through a series of compressor stages such as alow pressure stage and a high pressure stage. The air then passesthrough a combustion chamber and, in exiting the engine, crossesturbines such as high pressure and low pressure turbines. However, asignificant portion of air that enters the engine inlet passes aroundthe compressors, combustion chamber and turbines, this is called fanair. Additionally air in the compressors may be bled off for deicing andother pneumatic applications through bleed valves. Bleed valves aretypically used to select air at a desired pressure within the gasturbine engine during varying power conditions. Alternatively air may besupplied to the air craft cabin through a separate compressor notdirectly associated with the engine. Environmental control systems usedin commercial airliners often draw air from either the bleed valves orram air. This air may then pass through ductwork, pumps, temperaturecontrols, and other air handling equipment before being vented into thepassenger cabin.

Present in these turbine propulsion engines as well as the APU's(auxiliary power units) are fluid sealing systems. Sealing systemstypically work to contain materials such as lubricants and hydrocarbonswithin the engine body. For example sealing systems are employed withina gas turbine engine to prevent trace elements of materials such as fuelor lubricant from leaking from the engine and into the bleed air.However, such sealing systems are not always totally effective, and as aresult there may be leakage of fuel or lubricant into the bleed air.Hence hydrocarbons and lubricants within the engine may be the source ofsemivolatile compounds that result in odors and noxious impurities thatmay be harmful or unpleasant to the passengers. Hydrocarbons for examplecan oxidize and produce smoke and particulates in the air flowing intothe cabin.

Previous methods used to measure contaminants in engine bleed air haveeither been inconclusive or have given false readings. One such methodincorporates a polyvinylchloride filter to collect a sample of the bleedair followed by looking for the presence of oil by using a black lightto make the oil droplets fluoresce. Another method includes the use of alarge, stainless steel coil chilled to about −100 degrees F. to condensematter in the bleed air. The condensed matter is then flushed from thecoil, evaporated with a solvent (freon) and weighed. In a third method,the bleed air is flowed through absorption tubes in which residue iscollected on silica gel, charcoal, or molecular sieves and thenevaluated by gas chromatography/mass spectroscopy. The residue can alsobe analyzed by combusting its organic matter, and measuring the carbondioxide formed with a flame ionization detector or nitrogen phosphorousdetector.

Presently, there is no known equipment available that is designed tosample high volumes of air from a closed system. In particular there isno known equipment designed to take high volume air samples from theinterior chamber of a closed aircraft fuselage. Accordingly there is aneed for a high volume air sampler that can screen for particulate,volatile, and semivolatile materials present in the air sample.

In a closed environment, such as the fuselage interior of a commercialjet airplane, traditional methods of taking air samples facedifficulties. In the typical known method for taking air samples acollector is exposed to the environment where it is desired to take anair sample. One end of the collector is open to the atmosphere and anopposite end of the collector is attached to a pump (typically with anintervening hose). Running the pump pulls a vacuum which serves to pullair through the collector.

The difficulty of such an arrangement in a closed environment is thatpulling a vacuum to take the air sample is resisted by the closed natureof where the air sample is in the plane interior. Thus it is difficultto take large volume air samples with this arrangement. However, largevolume air samples are sometimes preferred where for example theconcentration of the suspected contaminant is relatively low. In such acase it is often necessary to sample a large volume of air in order tocapture a sufficient quantity of the contaminant in order to subject theimpurity to analysis.

Hence there is a need for a high volume air sampler that addresses oneor more of the above-noted objectives. That is there is a need for ahigh volume air sampler capable of drawing a sufficiently large airsample to detect the presence of certain airborne impurities; and/orthat is capable of drawing an air sample in a closed environment ofminimal weight and/or that is capable of drawing air samples that passthrough the enclosed interior of an airplane fuselage and/or that iscompact and portable so as to be used in different airplane shapes andsizes. The high volume air sampler disclosed herein addresses one ormore of these needs.

SUMMARY OF THE INVENTION

The present invention provides equipment and methods for samplingsemivolatile compounds in air from a low pressure air supply. Thepresent invention is particularly adapted to capturing an air samplefrom a low pressure air supply such as that provided by an airconditioning duct. The present invention is further adapted to capturingan air sample from the air supplied by air conditioning ductwork in apassenger airplane air conditioning system. The present inventionadditionally provides methods for using the air sampling equipment inthe airplane environment.

In one embodiment and by way of example only there is provided anapparatus for collecting an air sample from a vent comprising: acollection bag having an interior and an exterior, the collection bagfurther defining a collection opening and an exit; a means for affixing,such as a fastener or aluminum tape, the collection opening around anair conditioning vent; a tubing for conducting air having an upstreamend and a downstream end, the upstream end of the tubing affixed to theexit of the collection bag. The tubing may be affixed to the exit of thecollection bag so as to provide a substantially airtight sealtherebetween. The collection bag may comprise Teflon® or Tedlar®.Additionally the collection bag may further define an overflow escape. Avacuum source may be applied to the downstream end of the tubing.

In a further embodiment and by way of example only there is provided anapparatus for collecting an air sample from an aircraft air conditioningvent comprising: a flexible collection bag defining an interior, anexterior, a collection opening, and an exit; a fastener that affixes thecollection opening of said collection bag around an aircraft airconditioning vent; and a flexible tubing having an upstream end and adownstream end, and the upstream end of said tubing affixed to the exitof said collection bag. The flexible tubing may comprise in partaluminum tubing. The upstream end of the flexible tubing may be affixedto the exit of the collection bag with aluminum tape. Further thefastener may affix the collection opening of the collection bag aroundan aircraft air conditioning vent so as to prevent air from the exteriorof said collection bag, other than air provided by the vent, fromentering the interior of said collection bag through the collection bagopening. The downstream end of the flexible tubing may be affixed to asample canister.

In still a further embodiment also by way of example there is provided amethod for collecting an air sample from an aircraft air conditioningvent comprising the steps of: providing a collection bag having aninterior and a collection opening with the collection opening affixedaround an air conditioning vent; attaching a tubing with an upstream endand a downstream end to a collection bag exit at the tubing upstreamend; and applying a vacuum at the tubing downstream end. The method mayfurther comprise the step of providing air from an air conditioning ventto the interior of the collection bag, adjusting the vacuum so as toallow the collection bag to inflate, and adjusting the amount of airprovided from an air conditioning vent so as to allow the collection bagto inflate. In this method the airflow rate from the vacuum may be lessthan the airflow rate from the air conditioning vent. Also the methodincludes allowing air to escape from the interior of the collection bagthrough an overflow escape. The method may also comprise the step ofcollecting an air sample at a canister.

Other independent features and advantages of the high volume air samplerwill become apparent from the following detailed description, taken inconjunction with the accompanying drawings which illustrate, by way ofexample, the principles of the invention.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a schematic view of a high volume air sampler in accordancewith an embodiment of the invention.

FIG. 2 is a detailed view of a collar in accordance with an embodimentof the invention.

FIG. 3 is a schematic view of a high volume air sampler with a pressurereduction apparatus in accordance with an embodiment of the invention.

FIG. 4 is a detailed view of a pressure reduction apparatus inaccordance with an embodiment of the invention.

FIG. 5 is a schematic view of an air sampler with a collection bag inaccordance with an embodiment of the invention.

DETAILED DESCRIPTION OF A PREFERRED EMBODIMENT

Reference will now be made in detail to exemplary embodiments of theinvention, examples of which are illustrated in the accompanyingdrawings. Wherever possible, the same reference numbers will be usedthroughout the drawings to refer to the same or like parts.

High Volume Air Sampler

Referring now to FIG. 1 there is shown a schematic view of an embodimentof the high volume air sampler system. A preferred embodiment of thehigh volume air sampler system comprises multiple components. The highvolume air sampler begins with an air source. In one application of thesystem, the reference air supply source is a gas turbine engine 10 suchas found on a commercial airliner. The air supply may be taken, forexample, from fan air in the engine compartment. Alternatively andpreferably, the air is taken from a bleed valve 11 located on the engine10, or from a location within the aircraft environmental control system.Thirdly, air can be ducted from a confined location such as a cockpitair where there is insufficient room to locate a high volume collectionsystem.

Still referring to FIG. 1 source hose 20 draws air from bleed valve 11.Source hose 20 is preferably an electrically conductive flexible tubingsuch as for example flexible stainless steel or carbon loaded Teflontubing. Flexible conduit may be adapted and bent such that the tubingmay transport the air from the engine compartment, throughconfigurations in the aircraft body if necessary, to a desired location.

In one preferred embodiment, source hose 20 transfers air from bleedvalve 11 to a receptor. The receptor comprises collar 40 and a samplecanister 50.

Preferably the high volume air sampler is adapted to accept standardsized industry fittings for air sampling equipment. A three inchdiameter sampling system is one such preferred size. Thus source hose 20and collar 40 are preferably sized to accept such sized fittingsalthough other sizes are possible.

Referring now to FIG. 2 collar 40 comprises a structure whereby sourcehose 20 may be adapted to supply air to canister 50 through collar 40.In a preferred embodiment collar 40 is a hollow structure having aninterior and an exterior that allows fluid communication therethrough.Collar 40 includes body 43 clamp 44 and seal 46. Preferably collar 40 isconstructed in whole or part of a light, durable material such asaluminum or aluminum alloy. While collar 40 can be constructed invarious configurations, it is preferred to manufacture collar 40 fromaluminum tubing. When so manufactured, collar 40 is generallycylindrical in shape and circular in cross section.

Still referring to FIG. 2 collar 40 has an upstream end 41 and adownstream end 42. Collar 40 includes clamp 44 located at the downstreamend 42 of collar 40. In a preferred embodiment, the downstream end 40 ofcollar 40 includes lip 45. Lip 45 acts to retain clamp 44 on body 43 ofcollar 40. However, clamp 44 is free to rotate around body 43 of collar40. Lip 45 is preferably a knurl or curve fabricated in the aluminumtubing at the downstream end 42 of collar 40. Lip 45 preferably has adiameter greater than the diameter of clamp 43 whereby lip 45 works toretain clamp 44 on collar body 43. In a preferred embodiment, a gasket46 or sealing ring is disposed around collar body 43 between lip 45 andclamp 44. As shown, clamp 44 may include bolt holes 47 adapted toreceive fasteners (not shown) from canister 50. Fasteners such as boltsmay act to secure canister 50 to collar 40.

At various points in this description the system or components of thesystem are referred to with reference to an upstream or downstreamposition. Upstream refers generally to a direction or position towardthe air source such as the gas turbine engine 10 or bleed valve 11.Downstream refers generally to a direction or position toward the vacuumsource such as vacuum pump 70. In operation air flows through the systemin a generally upstream to downstream direction.

Still referring to FIG. 2 the upstream end 41 of collar 40 includes hosefitting 48. In a preferred embodiment, hose fitting 48 is a polymer orplastic fitting adapted to receive source hose 20. Preferably hosefitting 48 may comprise a polypropylene banjo clamp. Hose fitting 48 issecured to body 43 of collar 40. Preferably hose fitting 48 is glued tobody 43 of collar 40 to form a substantially airtight seal where hosefitting 48 attaches to body 43. Hose fitting 48 may itself includemating surface 49 adapted to receive source hose 20. When not in use, anend cap may be secured to end 41 ad retained via mating surface 49.

When hose fitting 48 is selected as a polypropylene banjo clamp, acorresponding banjo clamp may be used with the end of source hose 20that attaches to collar 40 to facilitate the attachment of source hose20 to collar 40.

As also shown in FIG. 2 collar may include one or more sample ports 39.Sample ports 39 are useful for taking air samples or for measuringconditions in the air at the interior of collar 40. A thermocouple orpressure gauge may be disposed at sample port 39 for measuring airconditions within collar 40.

In a preferred embodiment a sample port 39 is positioned on body 43 ofsaid collar 40. However, in a further embodiment a sample port may bepositioned at other locations in the high volume air sampling system.For example a sample port 39 may be positioned on source hose 20 ortubing 60. A sample port 39 is useful for measuring air conditions suchas temperature and pressure.

Referring now to the schematic of the high volume system shown in FIG. 1collar 40 is affixed to canister 50. Canister 50 represents any of thecommercially available or known sampling canisters used to collect ordetect airborne contaminants. For example, canister 50 may containreactive or adsorbent material. When contaminated air is passed throughcanister 50 airborne contaminants adhere to or otherwise react with thecontents of canister 50. In this way canister 50 can later be analyzedto determine the nature of the airborne contaminant. Further, ameasurement of the air volume passing through canister allowscalculation of the concentration of the airborne contaminant.

Downstream from canister 50 is tubing 60 that is connected to a vacuumsource such as vacuum pump 70. Tubing 60 provides the vacuum supply fromvacuum pump 70 to canister 50. Air may exit from the air sampling systemthrough vent 80.

In operation, source hose 20 is secured to collar 40. Source hose 20,having two ends, may be secured to collar 40 by affixing an end ofsource hose 20 at mating surface 49 of hose fitting 48. A preferredmeans of securing source hose 20 to hose fitting 48 includes use of aring clamp (not shown). Mating surface 49 acts to provide asubstantially airtight seal when source hose 20 is secured to collar 40.Source hose 20 is further disposed so that its other end is positionedto receive an air supply such as provided by bleed valve 11. In this waysource hose 20 transmits an air sample from an upstream position to adownstream position.

In operation clamp 44 of collar 40 is affixed to canister 50. The actionof affixing clamp 44 to canister 50 acts to press gasket 46 between lip45 and clamp 44 thereby resulting in a substantially airtight sealbetween collar 40 and canister 50. As a result air contamination of anair sample from the joint between collar 40 and canister 50 is minimal.

In operation an air sample is taken by drawing air from a turbineengine's bleed valve 11 or bleed valves. The bleed valve 11 provides airwhen the engine 10 is running. Preferably the equipment for the highvolume air sampler is attached before the engine 10 is operational. At adownstream position from the engine a vacuum source such as vacuum pump70 pulls air through the system. As the air sample passes through thesystem, the air will pass through canister 50. Impurities in the airreact with or otherwise are detected by canister 50. Canister 50 thusprovides a measurement of targeted impurities in the air sample.Alternatively, canister 50 may be further analyzed to determine thepresence and concentration of impurities in the air sample.

At various points in the description a seal or joint between systemcomponents is described as an airtight seal or a substantially airtightseal. Such a seal is not meant to be absolutely airtight so that no airwhatsoever will pass through the seal when the system is in operation.Rather an airtight seal or substantially airtight seal means such adegree of seal that air contamination through the seal does not affectthe analytical testing of the air sample in the system in anystatistically significant way. Any leakage of air through asubstantially airtight seal does not affect analysis of the air sample.

A first advantage of the high volume air sampler described herein is theability to take a high volume air sample from a high volume air supplyin a turbine jet engine using known and available sampling canisters.Additionally this advantage includes the ability to draw a high volumeair sample in an otherwise closed environment such as the interior of anairplane.

A further advantage of the high volume air sampler system describedherein is the ability to acquire an air sample with suspected impuritieswithout drawing in air from other sources that are not suspected to becontaminated. In other words the sampling system focuses the collectionof suspect air to the source of suspect air.

Still a further advantage of the air sampling system is the flexibilitywhereby suspect air may be gathered at a suspect engine or bleed valve.

Another advantage of the air sampling system is the inherentadaptability whereby flexible hose may be used to transport an airsample from a remote location, such as an engine compartment, to a moresuitable human work station for collection and analysis.

It is also advantageous that the air sampling system is portable andeasily used.

The materials used to construct the air sampling system are as describedor above or of other materials suitable for use with air handlingequipment.

Pressure Reduction Apparatus

In an alternative embodiment shown in FIG. 3, source hose 20 transfersair from bleed valve 11 to a pressure reduction apparatus 30 beforeproceeding downstream to collar 40 and other sampling equipment.

Air from the bleed valve or compressor section of a gas turbine engineis typically at a higher temperature and pressure than atmospheric air.The temperature and pressure conditions of bleed air may presentpractical challenges to the air handling equipment widely used fortaking and processing samples as well as safety hazards to the humanoperators using the equipment. In some embodiments it may be desirableto first reduce the temperature and pressure of the source air.

Source hose 20 provides a fluid conduit through which air from an airsource such as a turbine engine bleed valve 11 passes to pressurereduction apparatus 30. Source hose 20 should be of a dimension andmaterial adequate to provide the strength necessary to handle air atelevated temperatures and pressures. In aircraft engine applications thetemperature and pressure are those associated with various compressorstages of the turbine engine, which can vary depending on the enginetype. Material such as stainless steel may be used. However, it ispreferred that source hose 20 be constructed of a carbon impregnatedteflon or carbon impregnated silicone. These preferred materials assistin the avoidance of static charge buildup.

As shown in FIG. 4 one component of the high volume air sampler systemmay include pressure reduction apparatus or pressure reducer 30.Pressure reducer 30 comprises a hollow vessel defining an exterior 31and an interior 32 with apertures or ports providing fluid communicationbetween the exterior and the interior of said vessel. Various geometriesmay be used in constructing pressure reducer 30 including spherical,cubic, and other three dimensional configurations. In one embodiment,pressure reduction apparatus 30 is cylindrical or drum-like in shape. Ina preferred embodiment, pressure reduction apparatus 30 is comprised ofaluminum. Aluminum and other aeronautical alloys are preferred inairplane applications for weight considerations. Other metallic or rigidmaterials may also be used.

As shown in FIG. 4 pressure reduction apparatus 30 includes in oneembodiment inlet 33, outlet 34, and sample port 35. Air from the bleedvalve 11 or other air source is directed to the interior of pressurereduction apparatus 30 through inlet 33. Optionally, pressure reductionapparatus 30 may include other ports or apertures providing fluid accessto the interior of said apparatus.

Inlet 33, outlet 34, and sample port 35 may be of any dimension ordiameter. A three inch diameter size is preferred, however, as thismatches the dimension for common industrial air handling equipment.Also, preferably, sample port 35 inlet 33, and outlet 34 may include alip or protrusion (not shown) as a structure on which to attach anyflexible hose or line to such port.

Other equipment such as a valve, ball valve, one way valve or checkvalve may be included on any of the ports. In particular it is preferredthat ball valves be used at inlet 33 and sample port 35 so as to preventbackflow of air from the sample port 35 of pressure reduction apparatus30 to sample port 35 when sampling from inlet 33 at low pressure.Additionally, a pressure gauge 36 may be affixed to pressure reductionapparatus 30. Pressure gauge 36 may provide, for example, a digital oranalog read out of the interior pressure of pressure reductionapparatus. Likewise a thermocouple (not shown) or other temperaturesensitive device may also provide a reading of the temperature at achosen location such as the interior of the apparatus.

The dimensions of pressure reduction apparatus 30 are such that thetemperature and pressure of the air drawn from the apparatus throughoutlet 34 are reduced from the temperature and pressure of air that isadmitted into the apparatus through inlet 33. The degree of pressure andtemperature reduction may vary depending on the size and design of thepressure reduction apparatus. The pressure and temperature reductionachieved by the pressure reducer 30 is adequate to allow safe and propersampling and handling of the air sample by other equipment in the airsampling system. In a preferred embodiment the physical conditions ofthe air drawn from sample port are close to atmospheric pressures andtemperatures up to 150 deg. F.

When an air sampling system includes pressure reduction apparatus 30 anadditional hose or tubing will be required to transfer air from pressurereducer 30 to downstream equipment such as collar 40. FIG. 3 shows thisas transfer tubing 37. Transfer tubing 37 provides a channel throughwhich air is drawn from pressure reduction apparatus 30 and directed toany remainder of the air sampling system. Transfer tubing 37 can be thesame as source hose 20. Preferably transfer tubing 37 is a flexiblealuminum tubing of three inch diameter. This is stated as the preferredproperty for transfer tubing 37 as this represents a standard industrialsize for air handling equipment. Other dimensions and materials may bechosen. Flexible aluminum tubing allows easy movement and positioning oftransfer tubing 37.

In operation an air sample passes from an upstream position throughpressure reducer 30 to a downstream position. As an air sample enterspressure reducer 30, the air encounters an environment that allowsrelatively high pressure and high temperature air to expand in theinterior 32 of pressure reducer 30. In expanding, the air sample reducesin pressure and temperature. The air at reduced temperature and pressurethen exits pressure reducer to a downstream position.

If desired, pressure reducer may include supplemental cooling equipmentsuch as radiator fins and/or heat exchangers in order to remove heataccumulated within pressure reducer 30. In a preferred embodiment,pressure reducer 30 provides adequate cooling and heat exchange throughradiant heat loss from the surface area of pressure reducer.

A first advantage of the temperature reduction apparatus describedherein is the reduction in air temperature and pressure realized fromair drawn from a high volume source such as a gas turbine engine or ableed valve on a gas turbine engine.

A further advantage of the pressure reduction apparatus is the gain insafety realized from the temperature and pressure drop.

Still a further advantage of the pressure reduction apparatus is theability to use conventional air testing equipment upon the reduction intemperature and pressure realized by the device.

The materials that are used to construct the pressure reductionapparatus are as described herein or those suitable for use in theairline industry.

Air Sampling from Air Conditioning Vent

Referring now to FIG. 5 there is shown a schematic diagram of anembodiment of the apparatus used for sampling low pressure air with highvolume air collection equipment. An air source such as air conditioningvent 90 provides a source of air that is to be tested. In the passengerairplane environment one set of such air conditioning vents aretypically located along the wall of the fuselage above the windowsproximate to the passengers' heads. Collection bag 100 is positionedaround a vent 90 or set of vents from which it is desired to collect anair sample.

Collection bag 100 preferably defines a body 103 and two openings,collection opening 104 and exit 105. Collection bag 100 thus defines aninterior 101 and an exterior 102 relative to the collection bag.Collection bag 100 is formed of a material that prevents air that enterscollection bag_from escaping collection bag 100 through body 103. Air isfree to flow through collection opening 104 and exit 105. Furthercollection bag 100 is flexible and pliable so that its shape can beadapted to a variety of shapes and configurations.

Collection bag 100 is constructed of a durable and flexible material.Preferred materials are DuPont Tedlar® or Teflon®. Additionally materialchoice for collection bag 100 should minimize any residual hydrocarbonsor volatiles in the construction material itself. Preferably collectionbag 100 is made of an inert material that does not impart any volatilematerials into the air sample passing through the collection baginterior 101. In other words collection bag 100 material of constructionshould not affect the level of impurities in the air sample itself. Thusadditional preferred materials for construction of collection bag 100are polymeric and plastic materials provided that they have the requiredinertness and low volatiles. Metal/plastic laminates may also beutilized.

Collection opening 104 of collection bag 100 is adaptable to cover airconditioning vent 90. Thus the size of collection bag 100 and ofcollection opening 104 is somewhat dependent on the vent size to besampled. It has been found that collection bag 100 may be made of astandard size for ease of manufacturing and human handling. If a sizelarger than a standard size is required, multiple collection bags may bejoined together as described further below.

Referring again to FIG. 5 fastener 110 affixes collection bag opening104 around air conditioning vent 90. Preferably fastener 110 comprises atape material suitable for use on aircraft. A tape should be selectedthat provides good adhesion to both collection bag 100 and the airplanevent structure. Collection bag 100 is affixed around air conditioningvent 90 such that air exiting vent 90 passes to the interior 101 ofcollection bag 100. As indicated, collection opening 104 is positionedaround the particular vent or vent section from which it is desired todraw an air sample. Closure of collection opening 104 around vent 90 byfastener 110 prevents air from another source from entering collectionbag interior 101.

In a preferred embodiment, fastener 110 comprises an aluminum tape.Tapes and adhesives for use as fastener 110 should be selected andapplied in order to minimize any volatile materials or hydrocarbons thatmay otherwise enter the interior 101 of collection bag 100. The tackyportion of tape may include volatile materials. Nevertheless the methodof operation employed with the collection of air samples may minimizethe presence of such volatile materials in the air sample as describedbelow.

As further shown in FIG. 5 tubing 120 is affixed to collection bag 100at exit 105. Tubing 120 is affixed to collection bag 100 by fastener110. Again fastener 110 preferably comprises an aluminum tape aspreviously described. Tubing 120 comprises a hollow conduit to move anair sample gathered in collection bag 100 to a further downstreamposition. In a preferred embodiment tubing 120 comprises flexiblealuminum conduit. The flexibility of the conduit allows tubing 120 tosnake through different airplane configurations to a desireddestination.

Tubing 120 has two ends, a first end or upstream end, and a second,downstream end. Each end of tubing 120 has an opening. Tubing 120 allowsfluid movement therethrough. Upstream end of tubing 120 is affixed tocollection bag 100. Preferably the opening of tubing 100 at upstream endhas sufficient rigidity so that collection bag exit 105 can be affixedaround the upstream opening, and preferably this affixing or connectingis accomplished by fastener 110 such as tape. Thus upstream opening oftubing provides sufficient structure to withstand taping collection bagexit 105 to tubing. If necessary, fixtures or end pieces may be attachedto tubing 120 to provide a sufficiently rigid structure on which tofasten collection bag 100.

With respect to the high volume air sample there is described a tubing50, and with respect to the pressure reduction apparatus there isdescribed a tubing 37; additionally there is described a tubing 120 withrespect to use with collection bag 100. For clarification purposes it isnoted that each such tubing may be the same, a flexible aluminumconduit. Alternatively, each such tubing may be different. Preferably,tubing 50, tubing 37, and tubing 120 operate at temperatures andpressures lower than that used with source hose 20, and accordinglytubing 50, tubing 37, and tubing 120 may be different from source hose20.

Collection bag exit 105 preferably is fastened to tubing 120 so as toprovide a fluid passage between the interior 101 of collection bag 100and tubing 120. Preferably collection bag 100 is affixed to tubing 120so as to provide a substantially airtight seal. The seal betweencollection bag 100 and tubing 120 prevents air from a source differentfrom that provided by air conditioning vent 90 from entering into tubingthrough the tubing/collection bag joint.

Tubing 120 leads the air sample to a downstream point such as testingequipment as described herein, or other analysis equipment. Thus, tubing120 may be connected to collar 40 for providing an air supply to acanister 50. A vacuum source such as a vacuum pump 70 is included at apoint downstream of tubing 120. A vacuum supply to the downstream end oftubing 120 provides the necessary vacuum to draw an air sample providedby air conditioning vent 90 through collection bag 100 out of collectionbag exit 105 and into tubing 120.

In operation fastener 110 should preferably secure collection bag 100around vent 90 so as to prevent air from the collection bag exterior 102from being drawn into the collection bag interior 01 other than what airis supplied to the interior from vent 90. The application of tape oraluminum tape as fastener 110 should be done in a way to minimize thevolatile materials in the tape adhesive from appearing in the airsample. This is accomplished in part by minimizing the presence of anytape or adhesive in the interior 01 portion of collection bag 100.Volatiles are also limited in the way in which collection bag isinflated.

In use air is supplied at air conditioning vent 90 at a given rate offlow. In this manner air flows from vent 90 into the interior 101 ofcollection bag 100 and tends to inflate collection bag 100. The rate ofinflow from vent 90 can be controlled by operation of the aircraft's airconditioning system. Additionally, air is withdrawn from the interior101 of collection bag 100 through exit 105. Air is withdrawn by applyinga vacuum to tubing 120, as by a vacuum pump 70 attached to tubing 120whereby the vacuum operates on tubing 120 and collection bag 100. Therate of air withdrawal through exit 105 can be controlled by the levelof vacuum applied to collection bag 100. Preferably the rate of inflowinto collection bag interior 101 and the rate of outflow throughcollection bag exit 105 are controlled so that the interior 101 ofcollection bag remains in an inflated condition. Inflow is controlled toexceed outflow. In order to balance the greater flow of air coming fromvent 90 with the lesser flow of air passing out of exit 105, the methodmay further use an overflow escape 106. Overflow escape 106 may comprisea space where collection opening 104 is not secured to the airplanesurface thus providing a pathway for escape of excess air pressure fromcollection bag interior 101. Alternatively overflow escape 106 maycomprise a port or hole provided in body 103 of collection bag 100through which air may escape. Maintenance of collection bag 100 in aninflated condition in this way further assures that the air sample isbeing drawn from air supplied by vent 90 and not from any other airsource. Further the inflation of collection bag 90 provides a usefulvisual indication that the air sampling method is working properly.

As mentioned, in a preferred embodiment, collection bags aremanufactured in a given preferred size. This size may not accommodateall vent sizes, however. In such a situation multiple collection bagsmay be fastened together to reach the desired size. In this method, afirst collection bag is cut along body 103 beginning at collectionopening 104. A second collection bag is similarly cut along body 103also beginning at collection opening. The cut along each body creates afirst fold and a second fold in each collection bag. The firstcollection bag and second collection bag are then fastened togetheralong common folds. The result is that collection opening on each baghas been enlarged. This enlarged opening may then be fastened around theair conditioning vent.

The start up of the air sampling method may include a period foradjustments made to the airflow balance to assure proper inflation ofcollection bag 100. Additionally, once collection bag 100 has beeninflated, it may be desirable to run air through collection bag 100 fora period of time in order to purge any contaminants or volatiles thatmay have migrated to the interior 101 whether from a source such asfastener tape or non-targeted air. It may thus be desirable to delay theuse of any air sampling equipment such as canisters and PUF cartridgesuntil the proper air flow balance has been achieved within collectionbag and a purge period has passed. Once such start up conditions havepassed sampling equipment may then be attached to the sampling train ata position downstream of collection bag 100.

A first advantage of the apparatus and method for sampling air describedherein is the ability to collect a low pressure air sample using highvolume air sampling equipment. Additionally the apparatus may be adaptedto collecting an air sample from an air conditioning vent located on apassenger aircraft.

A further advantage of the apparatus and method described herein is thefact that the equipment is lightweight and adaptable to various aircraftconfigurations.

Still a further advantage of the apparatus and method described hereinis that an air sample may be taken from a particular air conditioningvent without contamination of that sample with air from another source.

Further, while the invention has been described with reference to apreferred embodiment or embodiments, those skilled in the art willunderstand that various changes may be made and equivalents may besubstituted for elements thereof without departing from the scope of theinvention. In addition, many modifications may be made to adapt to aparticular situation or material to the teachings of the inventionwithout departing from the essential scope thereof. Therefore, it isintended that the invention not be limited to the particular embodimentdisclosed as the best mode contemplated for carrying out this invention,but that the invention will include all embodiments falling within thescope of the appended claims.

1. An apparatus for collecting an air sample from a vent comprising: acollection bag having an interior and an exterior, said collection bagfurther defining a collection opening, an overflow escape, and an exit;means for affixing said collection opening around an air conditioningvent; and a tubing for conducting air having an upstream end and adownstream end, the upstream end of said tubing affixed to the exit ofsaid collection bag.
 2. The apparatus according to claim 1 wherein saidmeans for affixing comprise a fastener.
 3. The apparatus according toclaim 1 wherein said means for affixing comprise aluminum tape.
 4. Theapparatus according to claim 1 wherein said tubing is affixed to theexit of said collection bag so as to provide a substantially airtightseal therebetween.
 5. The apparatus according to claim 1 wherein saidcollection bag is comprised of Teflon® or other inert material.
 6. Theapparatus according to claim 1 wherein said collection bag is comprisesTedlar®.
 7. The apparatus according to claim 1 further comprising avacuum source applied to the downstream end of said tubing.
 8. Anapparatus for collecting an air sample from an aircraft air conditioningvent comprising; a flexible collection bag defining an interior, anexterior, a collection opening, an overflow escape, and an exit; afastener that affixes the collection opening of said collection bagaround an aircraft air conditioning vent; a flexible tubing having anupstream end and a downstream end, and the upstream end of said tubingaffixed to the exit of said collection bag.
 9. The apparatus accordingto claim 8 wherein said flexible tubing comprises in part aluminumtubing.
 10. The apparatus according to claim 8 wherein the upstream endof said flexible tubing is affixed to the exit of said collection bagwith aluminum tape.
 11. The apparatus according to claim 8 wherein saidfastener affixes the collection opening of said collection bag around anaircraft air conditioning vent so as to prevent air from the exterior ofsaid collection bag, other than air provided by the vent, from enteringthe interior of said collection bag through the collection bag opening.12. The apparatus according to claim 8 wherein the downstream end ofsaid flexible tubing is affixed to a sample canister.
 13. A method forcollecting an air sample from an aircraft air conditioning ventcomprising the steps of: providing a collection bag having an interiorand a collection opening with the collection opening affixed around anair conditioning vent; attaching a tubing with an upstream end and adownstream end to a collection bag exit at the tubing upstream end;applying a vacuum at the tubing downstream end; and allowing air toescape from the interior of the collection bag through an overflowescape.
 14. The method according to claim 13 further comprising the stepof providing air from an air conditioning vent to the interior of thecollection bag.
 15. The method according to claim 14 further comprisingthe step of adjusting the vacuum so as to allow the collection bag toinflate.
 16. The method according to claim 14 further comprising thestep of adjusting the amount of air provided from an air conditioningvent so as to allow the collection bag to inflate.
 17. The methodaccording to claim 14 wherein the airflow rate from the vacuum is lessthan the airflow rate from the air conditioning vent.
 18. The methodaccording to claim 13 further comprising the step of collecting an airsample at a canister.